Power control loop for stabilization of link power

ABSTRACT

The technology employs a state-based power control loop (PCL) architecture to maintain tracking and communication signal-to-noise ratios at suitable levels for optimal tracking performance and data throughput in a free-space optical communication system. Power for a link is adjustable to stay within a functional range of receiving sensors in order to provide continuous service to users. This avoids oversaturation and possible damage to the equipment. The approach can include decreasing or increasing the power to counteract a surge or drop while maintaining a near constant received power at a remote communication device. The system may receive power adjustment feedback from another communication terminal and perform state-based power control according to the received feedback. This can include re-initializing and reacquiring a link with the other communication terminal automatically after loss of power, without human intervention. There may be a default state and discrete states including rain, fade, surge and unstable states.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. application Ser. No.17/572,027, filed Jan. 10, 2022, the entire disclosure of which isincorporated herein by reference.

BACKGROUND

Certain types of communication terminals transmit and receive opticalsignals through free space optical communication (FSOC) links. In orderto accomplish this, such terminals may use acquisition and trackingsystems to establish the optical link by pointing optical beams fromdifferent terminals towards one another. For instance, a first,transmitting terminal may use a beacon laser to illuminate a second,receiving terminal. The receiving terminal may use a position sensor tolocate the transmitting terminal and to monitor the beacon laser.Steering mechanisms may maneuver the terminals to point toward eachother and to track the pointing once acquisition is established. A highdegree of pointing accuracy may be required to ensure that the opticalsignal will be correctly received.

Properties of the optical link can vary due to weather events, time ofday and other factors. This can adversely affect the signal-to-noise(SNR) ratio of the link. Power control may be employed in order tocorrect for changes in the SNR so that the received power is maintainedin a suitable range. However, it is possible to under-correct orover-correct, which may lead to saturation or damage to photodetectorsthat are sensitive to high peak irradiance. These and other issues withinadequate power control can degrade communication links of the FSOCsystem, reducing throughput and downgrading overall performance.

BRIEF SUMMARY

The technology employs a power control loop (PCL) architecture in orderto maintain tracking and communications laser SNRs at suitable levelsfor optimal tracking performance and optimal data throughput in an FSOCsystem, such as a terrestrial system having two or more wireless opticalcommunication terminals that may be positioned tens of kilometers apart.A state-lased algorithm is employed with adaptive setpoints and otherbeneficial features.

Optical communication channel properties may vary due weather events,e.g., over a large range such as up to 40 dB or more, and may fluctuateswith different day/night properties depending on link distance.According to aspects of the technology, an autonomous PCL correctionmechanism can be employed in such situations to maintain received powerin valid ranges (e.g., sufficient SNR satisfying one or more thresholdcriteria according to different setpoints). This approach allows fortargeted adjustments for both communication and beacon channels, and canavoid saturation and photodetector damage due to peak irradiance issues.

According to one aspect, a communication terminal is configured toreceive free space optical signals. The communication terminal comprisesa beam splitter, a position-sensing detector, an optical attenuator, apower monitoring block, and at least one photodiode. The beam splitteris configured to split an input optical beam received from anothercommunication terminal into a beacon wavelength and one or morecommunication wavelengths. The position sensing detector is configuredto receive the beacon wavelength from the beam splitter and to determinetarget tracking location information. The optical attenuator isconfigured to receive the one or more communication wavelengths from thebeam splitter and to attenuate at least one of the one or morecommunication wavelengths. The power monitoring block is configured toreceive the determined target tracking location information and tooutput a control signal to adjust the optical attenuator for theattenuation of the at least one of the one or more communicationwavelengths. The at least one photodiode is configured to receive theattenuated at least one communication wavelength and output one or moredetected communication signals. The power monitoring block is furtherconfigured to receive power adjustment feedback from a power controlblock of the other communication terminal and to perform state-basedpower control of the communication terminal according to the receivedpower adjustment feedback. The power monitoring block of thecommunication terminal may be further configured to receive the one ormore detected communication signals output by the at least onephotodiode.

The one or more communication wavelengths may comprise a plurality ofcommunication wavelengths. In this case, the at least one photodiode isa plurality of photodiodes each configured to receive one of theplurality of communication wavelengths, and the optical attenuator maybe configured to separately attenuate each of the plurality ofcommunication wavelengths. In this scenario, the communication terminalmay further comprise a demultiplexer configured to receive each of theplurality of communication wavelengths from the optical attenuator andto demultiplex the plurality of communication wavelengths prior toreception by the plurality of photodiodes.

The feedback may be an in-band optical signal. Alternatively, thefeedback may be an out-of-band radio frequency signal.

The power monitoring block may be configured, to calculate a center of afocused spot on a sensor plane for the input optical beam. Alternativelyor additionally, the power monitoring block may be further configured toprovide outbound power adjustment feedback to the power control block ofthe other communication terminal.

The received, power adjustment feedback may include at least one of aterminal control state, terminal motion, a power statistic, or atracking statistic.

Alternatively or additionally to any of the above arrangements, thestate-based power control may comprise a default state and multiplediscrete states including a rain state, a fade state, a surge state andan unstable state.

According to another aspect, a state-based method of controlling acommunication terminal configured to receive free space optical signalsis provided. The method comprises: splitting an input optical beamreceived from another communication terminal into a beacon wavelengthand one or more communication wavelengths; determining target trackinglocation information based on beacon information from the beaconwavelength; attenuating at least one of the one or more communicationwavelengths, the attenuation being adjusted based on the determinedtarget tracking location information; outputting one or more detectedcommunication signals based on the attenuated at least one of the one ormore communication wavelengths; receiving power adjustment feedback fromanother communication terminal; and performing state-based power controlof the communication terminal according to the received power adjustmentfeedback.

In one example, performing the state-based power control includesre-initializing and reacquiring a link with the other communicationterminal automatically after loss of power, without human intervention.The state-based power control may be performed based on (i) at least oneof a course pointing mirror angle or a fast steering mirror angle as astarting value, and (ii) at least one of an amplifier or an attenuatorsetting for power output. Alternatively or additionally, the state-basedpower control may include bounding output power based on at least one ofa distance from link setup or a channel temperature. Alternatively oradditionally, the state-based power control may comprise a default stateand multiple discrete states including a rain state a fade state, asurge state and an unstable state. Here, the multiple discrete statesmay further include an entry state during initial link acquisition,automated recovery or when the link is down due to an atmosphericcondition. Alternatively or additionally, operation in the rain stateincludes looking for an error in a tracking system of the communicationterminal where position feedback indicates that tracking satisfies aselected criterion but the communication terminal is unable to maintainsufficient light into a communication channel. Alternatively oradditionally, operation in the unstable state includes the communicationterminal reactively using variance of power information received fromthe other communication terminal to detect unstable tracking of theother communication terminal. Alternatively or additionally, operationin the fade state includes detecting when an update rate of control ofan attenuator or an amplifier of the communication terminal isinsufficient to stabilize received power for the other communicationterminal. Alternatively or additionally, operation in the surge stateincludes evaluating power saturation conditions associated with eitherthe communication terminal or the other communication terminal.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a block diagram 100 of an exemplary cot communication systemin accordance with aspects of the disclosure.

FIG. 2 is a pictorial diagram of components of the first communicationdevice and the second communication device of FIG. 1 in accordance withaspects of the disclosure.

FIG. 3 is a block diagram for an FSOC terminal in accordance withaspects of the technology.

FIG. 4 illustrates an example of active tracking in accordance withaspects of the technology.

FIG. 5 illustrates transmitter and receiver power optimization in a linkin accordance with aspects of the technology.

FIG. 6 is an example of state-based power control in accordance withaspects of the technology.

FIGS. 7A-B illustrate dynamic power adjustment from an operating linkwhile employing state-based power control in accordance with aspects ofthe technology.

FIG. 8 is a pictorial diagram of a network 800 in accordance withaspects of the disclosure.

FIG. 9 is a flow diagram 900 depicting a method in accordance withaspects of the disclosure.

DETAILED DESCRIPTION

Overview

The technology relates to a communication system configured to adjustthe power of a communication link based on disturbances to thecommunication system. Power for a link should be adjusted to stay withina functional range of receiving sensors in order to provide continuousservice to users. In particular, power should be high enough for thesensors to detect incoming signals but not so high so as to oversaturateand possibly damage the sensors in the communication system. Atmosphericangle-of-arrival and attenuation fluctuations, as well as pointing anglefluctuations introduced by a line-of-sight be tracking system, may causethe power received at as remote terminal to surge or drop. Thecommunication system may be able to decrease or increase the power tocounteract a surge or drop and maintain a constant or near constantreceived power at a remote communication device.

The features, described in more detail below, may provide for acommunication system that is able to maintain communication links atselected received power levels, even in variable environments. Thesystem may operate in highly-varying environmental conditionsautonomously without human intervention. There are several automationfeatures that provide operational robustness and resilience in thefield. For instance, the system can support automatic adjustment oftransmitter power over, e.g., a 30 dB dynamic range (or more or less),as channel attenuation varies due to changing weather conditions. It maybe configured to monitor averaged incident power at receiverphotodetectors to provide automated conditioning of received opticalpower. The system may also enable automatic restart and reacquisition ofa link after a long outage (e.g., due to power loss or fog).

An FSOC system as described herein may be, in one scenario, aterrestrial-based system having two or more wireless opticalcommunication terminals arranged at different locations. By way ofexample, this can support existing terrestrial broadband infrastructure,and enable access to abundant and affordable broadband internet tounder-connected populations across the world. In one particularsituation, the system may provide up to 20 Gbps (gigabit-per-second)bidirectional full-duplex throughput, with up to 20 km of line-of-sight(LOS) deployment, where a relay configuration for non-LOS can also besupported. In this configuration, the system may employ laserwavelengths operating in the near-infrared spectrum around 1550 nm(e.g., +/− up to 10%) with class 1M eye safe at the aperture, usingsmall low-power FSOC terminals that can be easily deployed. Forinstance, the terminal itself (absent mounting hardware) may be lessthan about 15 kg, with a typical power consumption on the order of 40 W,up to a maximum of 60 W.

In this example scenario, the system may employ on-off keying (OOK)modulation and direct detection, with dual-stage continuous activeline-of-sight tracking. There may be orders of magnitude reserve powermargin (e.g., approximately 45 dB at 10 km) to maintain operational linkthrough poor visibility conditions. The system supports automaticadaptation of link parameters to variations in the environmentalconditions (e.g., transmitter power optimization, acquisition andre-acquisition of link, auto-recovery from power loss), as well as usingan adaptive throughput modem with Automatic Repeat Request (ARQ)protocol for immunity against burst errors. The system may also providesupport for hybrid radio frequency-wireless optical communication(RF-WOC) or optical fiber-WOC architectures for additional availability.

Example Systems

General Terminal Architecture

FIG. 1 is a block diagram 100 of a first communication device 102 of afirst communication terminal configured to form one or more links with asecond communication device 130 of a second communication terminal, forinstance as part of a free-space optical communication (FSOC) system. Inthis example, the first communication device 102 includes as componentsone or more processors 104, a memory 106 storing data 108 andinstructions 110, a transmitter 112, a receiver 114, a steelingmechanism 116, and one or more sensors 118. The first communicationdevice 102 may include other components not shown in FIG. 1 .

The one or more processors 104 may be hardware-based processors, such ascommercially available central processing units (CPUs), microcontrollersor digital signal processors (DSPs). Alternatively, the one or moreprocessors may be a dedicated device such as an application specificintegrated circuit (ASIC) or other hardware-based processor, such as afield programmable gate array (FPGA). Although FIG. 1 functionallyillustrates the one or more processors 104 and memory 106 as beingwithin the same block, the one or more processors 104 and memory 106 mayactually comprise multiple processors and memories that may or may notbe stored within the same physical housing. Accordingly, references to aprocessor or computer will be understood to include references to acollection of processors or computers or memories that may or may notoperate in parallel.

Memory 106 may store information accessible by the one or moreprocessors 104, including the data 108 and instructions 110, which maybe executed by the one or more processors 104. The memory may be of anytype capable of storing information accessible by the processor,including a computer-readable medium such as a hard-drive, memory card,ROM, RAM, DVD or other optical disks, as well as other write-capable andread-only memories. The system and method may include differentcombinations of the foregoing, whereby different portions of the data108 and instructions 110 are stored on different types of media. In thememory of each communication device, state information may be stored,such as state information for tracking a signal and performing powercontrol as discussed herein.

Data 108 may be retrieved, stored or modified by the one or moreprocessors 104 in accordance with the instructions 110. For instance,although the technology is not limited by any particular data structure,the data 108 may be stored in computer registers, in a relationaldatabase as a table having a plurality of different fields and records,XML documents or flat files.

The instructions 110 may be any set of instructions to be executeddirectly (such as machine code) or indirectly (such as scripts) by theone or more processors 104. For example, the instructions 110 may bestored as computer code on the computer-readable medium. In that regard,the terms “instructions” and “programs” may be used interchangeablyherein. The instructions 110 may be stored in object code format fordirect processing by the one or more processors 104, or in any othercomputer language including scripts or collections of independent sourcecode modules that are interpreted on demand or compiled in advance.Functions, methods and routines of the instructions 110 are explained inmore detail below, for instance regarding a state-based algorithmconfigured to implement a power control loop.

The one or more processors 104 are in communication with the transmitter112 and the receiver 114. Transmitter 112 and receiver 114 may be partof a transceiver arrangement in the first communication device 102. Theone or more processors 104 may therefore be configured to transmit, viathe transmitter 112, communication data and/or beacon information viaone or more signals, and also may be configured to receive, via thereceiver 114, communication data and/or beacon information in one ormore other signals. The received signal(s) may be processed by the oneor more processors 104 to extract the communications data and/or beaconinformation.

As shown in FIG. 1 , the transmitter 112 of the first communicationdevice 102 is configured to output a beacon beam 120 to establish acommunication link 122 with the second communication device 130, whichreceives the beacon beam 120. The first communication device 102 mayalign the beacon beam 120 co-linearly with the optical communicationbeam (not shown) that may have a narrower solid angle or the same angleas the beacon beam 120 and carries a communication signal 124. As such,when the second communication device 130 receives the beacon beam 120,the second communication device 130 may establish a line-of-sight linkwith the first communication device 102 or otherwise align with thefirst communication device. As a result, the communication link 122 thatallows for the transmission of the optical communication beam (notshown) from the first communication device 102 to the secondcommunication device 130 may be established.

The transmitter 112 may include an optical transmitter, an amplifier,and an attenuator. As shown in the example architecture 200 of FIG. 2 ,the transmitter 112 of communication device 102 includes a seed laser202 configured to provide an amount of bandwidth for an output signal,an amplifier 204 such as an Erbium-doped fiber amplifier (EDFA)configured to increase an amplitude of the output signal(s) from theseed laser 202, and an attenuator 206 such as a variable opticalattenuator (VOA) that may be a single mode variable optical attenuator(SMVOA) or a multi-mode VOA (MMVOA) that is configured to decrease theamplitude of the output signal. The output of the attenuator 206 is fedinto the amplifier 204 along with the seed laser output signals. Viathis architecture, the transmitter 112 may be configured to output thebeacon beam 120 that allows one communication device to locate another,as well as one or more communication signals over one or morecommunication links 122. The output signal from the transmitter 112 maytherefore include the beacon beam 120, the communication signal(s) 122,or both. The communication signal(s) may be a signal configured totravel through free space, such as, for example, an RF signal or anoptical signal as shown by propagation path 208. In some cases, thetransmitter includes a separate beacon transmitter configured totransmit the beacon beam and one or more communication link transmittersconfigured to transmit the optical communication beam. Alternatively,the transmitter 112 may include one transmitter configured to outputboth the beacon beam and the communication signal. The beacon beam 120may illuminate the same or a larger solid angle in space than theoptical communication beam used in the communication link 122, allowinga communication device that receives the beacon beam to better locatethe beacon beam. For example, the beacon beam carrying a beacon signalmay cover an angular area on the order of a square milliradian, and theoptical communication beam carrying a communication signal may cover anangular area on the order of a hundredth of a square milliradian.

The receiver 114 of communication device 102 includes a tracking systemconfigured to detect a received optical signal from a remotetransmitter. As shown in FIG. 2 , the receiver 114 for the opticalcommunication system may include an attenuator 210 such as a multi-modevariable optical attenuator or a single mode variable optical attenuatorconfigured to adjust an amplitude of a received signal, a photosensitivedetector 212, and/or a photodiode 214. Using the photosensitive detector212, the receiver 114 is able to detect a signal location and convertthe received optical signal from propagation path 216 into an electricsignal using the photoelectric effect. The receiver 114 is able to trackthe received optical signal, which may be used to direct the steeringmechanism 116 to counteract disturbances due to scintillation and/orplatform motion. The system may process the signal output from thephotosensitive detector 212 by, e.g., performing integration, low-passfiltering and/or window-based sampling. In the example of FIG. 2 , theresultant signal is combined with output from the attenuator 210 andphotodiode 214 at block 218. The combined signal may then be processedby a controller 220, and its output controls operation of the seed laser202 and attenuator 206. For instance, each communication channel couldbe adjusted independently as well, for example, by adjusting the seedlaser powers for each channel.

Returning to FIG. 1 , the one or more processors 104 are incommunication with the steering mechanism 116 for adjusting the pointingdirection of the transmitter 112, receiver 114, and/or optical signal.The steering mechanism 116 may include one or more mirrors that steer anoptical signal through the fixed lenses and/or an adjustment mechanism(e.g., a gimbal) configured to move the transmitter 112 and/or thereceiver 114 with respect to the communication device. In particular,the steering mechanism 116 may be a MEMS 2-axis mirror, 2-axis voicecoil mirror, or piezoelectric 2-axis mirror. The steering mechanism 116may be configured to steer the transmitter, receiver, and/or opticalsignal in at least two degrees of freedom, such as, for example, yaw andpitch. The adjustments to the pointing direction may be made to acquirea communication link, such as communication link 122, between the firstcommunication device 102 and the second communication device 130. Toperform a search for a communication link, the one or more processors104 may be configured to use the steering mechanism 116 to point thetransmitter 112 and/or the receiver 114 in a series of varyingdirections until a communication link is acquired. In addition, theadjustments may optimize transmission of light from the transmitter 112and/or reception of light at the receiver 114.

The one or more processors 104 are also in communication with the one ormore sensors 118. The one or more sensors 118 are configured to monitora state of the first communication device 102. The one or more sensorsmay include, by way of example, an inertial measurement unit (IMU),encoders, accelerometers, and/or gyroscopes configured to measure one ormore of pose, angle, velocity, torques, as well as other forces actingon the terminal. In addition, the one or more sensors 118 may includeone or more sensors configured to measure one or mute environmentalconditions such as, for example, temperature wind, radiation,precipitation, humidity, etc. In this regard, the one or more sensors118 may include thermometers, barometers, hygrometers, etc. While theone or more sensors 118 are depicted in FIG. 1 as being in the sameblock as the other components of the first communication device 102, insome implementations, some or all of the one or more sensors may beseparate and remote from the first communication device 102.

The second communication device 130 includes one or more processors 132,memory 134 storing data 136 and instructions 138, a transmitter 140, areceiver 142, a steering mechanism 144, and one or more sensors 146. Theone or more processors 132 may be similar to the one or more processors104 described above. Memory 134 may store information accessible by theone or more processors 132, including data 136 and instructions 138 thatmay be executed by the processor(s). Memory 134, data 136, andinstructions 138 may be configured similarly to memory 106, data 108,and instructions 110 described above. In addition, the transmitter 140,the receiver 142, the steering mechanism 144 and the sensors 146 of thesecond communication device 130 may be similar to the transmitter 112,the receiver 114, and the steering mechanism 116 described above.

Like the transmitter 112, transmitter 132 may include an opticaltransmitter, an amplifier, and an attenuator. As shown in FIG. 2 , thetransmitter 132 of communication device 130 includes a seed laser 222configured to provide an amount of bandwidth for an output signal, anamplifier 224 such as an EDFA configured to increase an amplitude of theoutput signal, and an attenuator 226, e.g., a SMVOA or MMVOA configuredto decrease the amplitude of the output signal. As shown in FIG. 2 ,amplifier 224 causes the output signal to be sent along the propagationpath 216. As noted above for communication device 102, eachcommunication channel sent from communication device 130 could beadjusted independently as well, for example, by adjusting the seed laserpowers for each channel. Additionally, as shown in FIG. 1 , transmitter140 may be configured to output both an optical communication beam and abeacon beam. For example, transmitter 140 of the second communicationdevice 130 may output a beacon beam 126 to establish a communicationlink 128 with the first communication device 102, which receives thebeacon beam 126. The second communication device 130 may align thebeacon beam 126 co-linearly with the optical communication beam (notshown) that may have a narrower solid angle or the same angle as thebeacon beam and caries another communication signal. As such, when thefirst communication device 102 receives the beacon beam 126, the firstcommunication device 102 may establish a line-of-sight with the secondcommunication device 130 or otherwise align with the secondcommunication device. As a result, the communication link 128, thatallows for the transmission of the optical communication beam (notshown) from the second communication device 130 to the firstcommunication device 102, may be established.

Like the receiver 114, the receiver 142 includes a tracking systemconfigured to detect an optical signal as described above with respectto receiver 114. As shown in FIG. 2 , the receiver 114 for the opticalcommunication system of communication device 130 may include anattenuator 228, such as a single mode or multi-mode variable opticalattenuator configured to adjust an amplitude of a received signal, aphotosensitive detector 230, and/or a photodiode 232. Other componentssimilar to those pictured in the first communication device 102 may alsobe included in the second communication device 130. For instance, usingphotosensitive detector 230, the receiver 142 is able to detect a signallocation and convert the received optical signal into an electric signalusing the photoelectric effect. As shown in the example of FIG. 2 ,signals from the photosensitive detector 230 and photodiode 232 arecombined at block 234, and passed to both seed laser 222 and attenuator226. The receiver 142 is able to track the received optical signal,which may be used to direct the steering mechanism 144 to counteractdisturbances due to scintillation and/or platform motion.

Returning to FIG. 1 , the one or more processors 132 are incommunication with the steering mechanism 144 for adjusting the pointingdirection of the transmitter 140, receiver 142, and/or optical signal,as described above with respect to the steering mechanism 116. Theadjustments to the pointing direction may be made to establishacquisition and connection link between the first communication device102 and the second communication device 130. In addition, the one ormore processors 132 are in communication with the one or more sensors146, such as is described above with respect to the one or more sensors118. The one or more sensors 146 may be configured to monitor a state ofthe second communication device 130 in a same or similar manner that theone or more sensors 118 are configured to monitor the state of the firstcommunication device 102.

As shown in FIG. 1 , the communication links 122 and 128 may be formedbetween the first communication device 102 and the second communicationdevice 130 when the transmitters and receivers of the first and secondcommunication devices are aligned, or in a linked pointing direction.Using the communication link 122, the one or more processors 104 cansend communication signals to the second communication device 130. Usingthe communication link 128, the one or more processors 130 can sendcommunication signals to the first communication device 102. In someexamples, it is sufficient to establish one communication link betweenthe first and second communication devices, which allows for thebi-directional transmission of data between the two devices. Thecommunication links in these examples are FSOC links. In otherimplementations, one or more of the communication links may beradio-frequency communication links or other type of communication linkcapable of traveling through free space.

Terminal Configurations

FIG. 3 illustrates a block diagram of an example configuration 300 foran FSOC terminal in accordance with aspects of the technology. While notintending to be limiting in any manner, in this example the terminal mayhave a monostatic design with a single 75 mm clear aperture for opticaltransmission and reception. Here, the terminal may emit three (or more)laser wavelengths (e.g., two (or more) for 10 Gbps telecom signals, andone beacon dedicated to tracking), and similarly receives three (ormore) laser beams at different wavelengths (all of which may be within100 nm of 1550 nm). Note that the signals transmitted on each wavelengthmay have different throughput and/or different modulation formats.Dashed lines in FIG. 3 indicate paths of laser beams received by andoutput from the terminal.

The receiver path is as follows. Three laser beams are incident on aterminal aperture window 302, which is desirably hydrophobically- andanti-reflection-coated, and then on a coarse pointing mirror (CPM) 304.The beams reflected off the CPM 304 go through a telescope withapproximately 40× demagnification. The telescope in this exampleincludes a first lens 306 a and a second lens 306 b. At the conjugateplane in the demagnified space, the beams are incident on a faststeering mirror (FSM) 308.

After reflecting off of the mirror 308, the beams are incident on adichroic beam splitter 310, which reflects the beacon wavelength andtransmits the two communications laser beams. The beacon laser thatreflects off of the dichroic mirror is focused by lens 312 onto aposition-sensing detector (PSD) 313, from which the center of thefocused spot on the sensor plane can be calculated by a pointing,acquisition and tracking (PAT) module 314, such as a DSP. This input andinformation from one or more external sensors, as shown by dotted arrow316, is used by the PAT module 314 as feedback for adjusting thepointing direction of the two mirrors (the CPM 304 and FSM 308). Thebeacon laser may be modulated at a low frequency (e.g., on the order of1-3 KHz, or more or less) to allow for optical background and clutterrejection via narrowband filtering around the modulation frequency inthe receiver processing chain, prior to computing the center of thesignal beam.

The telecommunications beams (two wavelengths) that are transmittedthrough the dichroic beam splitter 310 are focused onto a fiber such asa multimode receiver fiber (dashed double arrow 320) via a collimatorlens 318. The fiber-coupled beams are directed through a circulator 322towards the receiver photonics components. Here, the beams may be firstconditioned via an actively-controlled multimode variable opticalattenuator (VOA) 324 to ensure the incident power on the downstreamphotodetectors are at an optimal threshold. Next, the telecommunicationswavelengths are demultiplexed and filtered at block 326, and thendetected via high-bandwidth and high-sensitivity avalanche photodiodesat blocks 328 a and 328 b. Post detection, the signals may be amplified,conditioned, and converted to bits via clock and data recovery (notshown). At block 330, a high-speed modem processor is configured toextract the data packets from the communication signals (e.g.,Ethernet-type telecommunication signals) and send them out on one ormore fiber-optic client ports 332.

The transmitter path is predominantly the reverse of the receiver path.For instance, client-side Ethernet or other communication traffic entersthe terminal through one or more fiber optic ports 334. At block 330,the modem processor is configured to structure packets into frames thatare optimized for transmission over the wireless optical channel. Theframes of each communication channel are processed independently andthen intensity modulated onto two seed lasers at block 336 a and 336 b.Beacon power can be adjusted relative to the communication beams via avariable optical attenuator (VOA) 340. The two laser beams, along withbeacon laser beam generated at block 338 prior to VOA 340, are combinedin a multiplexer 342. The combined three wavelengths in a single modefiber (shown as dotted arrow 344) are amplified in an Erbium-dopedoptical amplifier (EDFA) 346, and then propagated into the third port ofthe circulator 322, such that they are emitted into free space from thesame port that receives the light in the receiver path via terminalaperture window 302.

In this example architecture, the circulator 322 has three ports: a dualsingle- and multi-mode core bidirectional port that faces free space, amultimode receiver output port, and a single-mode transmitter inputport. This circulator enables the system to operate in a monostaticconfiguration with single-mode transmission, yet, multimode reception,which is advantageous for terrestrial communications wherein theatmosphere causes significant wavefront and irradiance distortions. Thethree transmit beams traverse the optical path inside the terminal inthe opposite direction, reflecting off the FSM 308 and the CPM 304, andthen exit the terminal through the aperture 302. Dash-dot arrow 348indicates that the PAT module 314 is configured to adjust the CPM 304,and dotted arrow 350 indicates that the PAT module 314 is alsoconfigured to adjust the FSM 308.

The line of sight between two terminals can be maintained by two-stageactive tracking. The Coarse Pointing Mirror (CPM 304 in FIG. 3 ) has aprimary responsibility to compensate for disturbances that are large inangle (e.g., on the order of degrees) but rather low in frequency (e.g.,on the order of 1 Hz or lower). Examples include mount motion due todiurnal temperature changes or low frequency swaying of the pole due towind. The fast steering mirror (FSM 308 in FIG. 3 ) compensates fordisturbances that are high in frequency (˜tens of Hz), but small inabsolute angular range (e.g., on the order of tens-to-hundreds ofμrads). Examples include vibrations from nearby equipment or higherfrequency excitations in the mounting structure from wind.

A controller (e.g., of PAT module 314) for the two-stage active trackingsystem can be described by the example 400 in the block diagram of FIG.4 . The tilt angle of beams entering a terminal have one-to-onecorrespondence to the center of the spot incident on theposition-sensing detector (313 in FIG. 3 ). The signals obtained by thisdetector are first passband-filtered around the modulation frequency toreject out-of-band background and clutter, then demodulated to baseband,followed by processing to estimate the center of the spot. Theseestimates inform the controller (PAT module 314) of changes to theincidence angle of the beams arriving from the remote terminal due toplatform motion (θ_(p)(t)) as well as atmospheric beam wander(θ_(c)(t)). A proper integration time is critical to obtain estimateswith adequate signal-to-noise ratio. In one scenario, the beam-centerestimates may be updated at the rate of hundreds of Hz, or more or less.

The difference between the beam-center estimate and the target trackinglocation on the position-sensing detector (corresponding to the opticalboresight of the system) is the error signal (tilt measurement-targetangle) that is input to the controller of PAT module 314. Thiscontroller is configured to command signals for the FSM 308 and CPM 304of the pointing assemblies (plant) to try to drive the error signal tozero (or otherwise as low as possible). The resulting actuation of thesetwo mirrors changes the arrival (and departure) angle of the laser beams(see resultant pointing angle θt)) and closes the feedback loop.

According to one scenario, the terminals providing free-space opticalcommunication can be deployed as telecommunications devices that passtraffic arriving through the fiber-optic client Ethernet ports. Forinstance, there may be multiple communication channels, each running10G-base Ethernet independently from input to output. The modem core mayemploy forward error correction and hybrid automatic repeat request(ARQ) to ensure robust communication through the turbulent atmosphere.Note that there may be separate modem instances for each channel.

Automated Power Control

As noted above, terminals according to the technology described hereinmay operate in highly-varying environmental conditions autonomouslywithout human intervention. In order to accomplish this, the system isable to implement the following automation features.

One such feature is the automatic adjustment of transmitter power over,e.g., 30 dB dynamic range in some examples, or between 20 dB to 45 dB(or more) in other examples, as channel attenuation varies due tochanging weather and/or other conditions. Terminal pairs in a link areconfigured to exchange necessary information about the state of theirsystems to enable automatic and dynamic optimization of the transmittedoptical power for robust link operation.

FIG. 5 illustrates an example block diagram 500 of transmitter andreceiver power optimization in a link. Each terminal monitors key systemparameters and exchanges state information with the other terminal toadjust operating setpoints. In this illustration, only the transmit pathis shown for a first terminal 502, and only the receive path is shownfor a second terminal 520. Here, beacon transmit signal 504 and thecommunication transmit channels 506 a and 506 b are combined viamultiplexer 508 (such as multiplexer 342 discussed above with regard toFIG. 3 ). The beacon transmit signal 504 is attenuated by attenuator510, e.g., a variable optical attenuator (such as VOA 340 of FIG. 3 )prior to multiplexing. As discussed above with regard to FIG. 3 , thewavelengths of these signals may be combined in, e.g., a single modefiber and may then be amplified in an optical amplifier 512 (such as anEDFA), and then subsequently emitted as shown by dotted line 514 fortransmission into free space via the aperture window of the firstterminal. As illustrated in FIG. 5 , a power control block 516 can causeadjustments to the attenuator 510 via a signal 518.

On the receive side, the second terminal 520 receives a free spaceoptical signal via its aperture window. After passing through theoptical elements discussed above for FIG. 3 , the input beams 522 areincident on a beam splitter 524 such as a dichroic beam splitter, whichreflects the beacon wavelength and transmits the two communicationslaser beams. The beacon laser that reflects off of the dichroic mirroris focused onto a position-sensing detector (PSD) 526, which passes theresultant information 528 to a power monitoring block 530 (of, e.g., thetracking (PAT) module 314 of FIG. 3 ). The power monitor block 530 isconfigured to output a control signal 532 to adjust optical attenuator534 (e.g., VOA 324 of FIG. 3 ). The attenuated communication signal(s)from the optical attenuator 534 are demultiplexed and filtered at block536. The signals are then detected via high-bandwidth andhigh-sensitivity avalanche photodiodes at blocks 538 a and 538 b. Postdetection, the outputs of the photodiodes may be provided to the powermonitoring block 530 (in addition to being processed by a high-speedmodem processor as discussed above with regard to block 330 of FIG. 3 ).Then, as shown by arrow 540, the power monitoring block 530 of thesecond terminal 520 is able to provide power adjustment feedback to thepower control block 516 of the first terminal. This feedback may be,e.g., in band (optical) or out of band (RF).

Automated State-Based Power Control

For automated conditioning of received optical power, the system canactively monitor short-time-averaged power incident on the receiverphotodetectors, and control the variable optical attenuator at a rate onthe order of KHz (e.g., 1 KHz-5 KHz, or more or less) to maintainoptimal power levels for operation in the presence of fast powerfluctuations (e.g., scintillation or rain). This compresses the dynamicrange of observed power fluctuations, can also ensure photodetectors arenot damaged from excessive incident power and can keep the tracking beamwith the stable bounds of accurate position detection.

The system is also able to perform an automatic restart andreacquisition of a link after a long outage (e.g., due to power loss orfog). For instance, poor visibility conditions could result in hour-longoutages where the attenuation along the link is too severe to close alink. In these instances, the terminals may automatically save the lastknown operating state of the link (e.g., pointing angles for the CPM andFSM, power levels for the transmitter), and then periodically(asynchronously) attempt to reacquire the link when the weatherconditions improve. The state information is used as either initialconditions or as inputs for the reacquisition process. Thus, theterminals are able to use the state information to re-initialize andreacquire a link automatically after loss of power, without humanintervention. By way of example, CPM and FSM angles may be used directlyby a controller as starting values, but power output (e.g., EDFA and/orVOA settings) may be suggested inputs. Various parameters (e.g.,distance from link setup, or channel temperature and/or otherenvironmental factors) determine how to bound the output power tomaintain safe operation. In this example, if output power is less than athreshold that's a function of parameters, the controller may keep theoriginal power; however, if the power is greater than a threshold that'sa function of parameters, it may limit the power to some bounded value.

In a non-state-space approach, the process takes physical layermeasurements as inputs and outputs a new power setpoints. In thisapproach, there is no notion of a “state” that the system is in.However, a more robust approach is state-based. Here, the behaviorsdepend on the environment and various states of both terminals (asopposed to just power in a stateless approach). For instance, examplesof additional data sent over from the receive terminal to thetransmitter terminal can include one or more of the following: terminalcontrol state, terminal motion, power statistics, tracking statistics,etc. There can be different system behaviors based on changes inenvironmental conditions. For instance, there may be a “Wind” state,which gives less weight to average power measurements due to reducedaccuracy in the measurements due to swaying or other movement of theterminal caused by the wind, or instability of the tracking systemcaused by fast fluctuations of the received power. A “Rain” state mayresult in modifying the behavior of the power control algorithm to takeinto account additional tracking jitter caused by the presence ofscattering light from rain. Both types of states may cause a change tothe power adjustment behavior.

One or more adaptive setpoints can be used to make adjustments to beaconpower (for a tracking system) based on information from thecommunication link (e.g., communication throughput and error rate). Thisadds resilience and robustness to device-to-device variations inperformance (e.g., power vs. sensitivity may be different for eachterminal), as well as a more direct measure of environmental conditions(e.g., the method is resilient to the channel causing changes to thereliability of physical layer measurements such as the average power).

The adaptive setpoints are also able to adjust the communication linkpower setpoint, depending on the fraction of observed outages. Forinstance, one goal may be to keep the lowest setpoint of the two, suchthat outages are <1% in order to provide substantially error-freecommunication. This is based off of the forward error correction (FEC)error rate. In one scenario, the setpoint adjusts over time with a smalldecay factor (a “forgetting” factor) multiplying the power error fromthe desired setpoint, to allow the communication link power setpoint tocontinually adjust while remaining as low as possible to maintainsuitable communication, which allows maximum power to the trackingsystem's beacon. Allowing the communication link power setpoint to be aslow as possible can provide an additional benefit of extending theoperational life of electro-optic components including lasers andoptical amplifiers. After some time, the forgetting factor causes thesetpoint to revert to its default state, with a time constant correlatedwith known channel fluctuations caused by nominal atmosphericscintillation and pointing jitter. Certain state transitions may alsocause the setpoint to revert as well, so that the system does notre-acquire the link in calm conditions with an extremely high setpointthat was needed previously but which is not needed in presentconditions. Thus, according to one aspect, the maximum increase of thedynamic setpoint can be limited to prevent highly dynamic situationsfrom causing into increase to a level that could result in damage tocomponents of the terminal.

In view of this, the state-based approach provides a power adjustmentloop that attempts to maintain tracking and communications laser SNR ata suitable level for optimal tracking performance, and optimal datathroughput (respectively). Thus, as channel properties vary due toweather conditions over a large range (e.g., on the order of up to 40 dBor more), and fluctuates with different day/night properties dependingon link distance, the power control loop provides an autonomouscorrection mechanism to maintain received power in valid ranges(sufficient SNR above an operating threshold). This helps to avoidsaturation and damage to sensitive photodetectors.

For the tracking beacon received power, the desired receive setpoint maybe selected such that expected scintillation does not commonly causefades (when the power drops below noise threshold) or surges (when thepower increases beyond bias-free level). For the communications laserreceived powers, the desired receive setpoint may be selected such thatexpected scintillation does not cause power to drop below the forwarderror correction (FEC) error threshold for which error-freecommunication is available.

Thus, it can be seen that there are two different setpoints. Thestate-based power control loop is configured to control power to thebeacon and communication channels independently, e.g., via a SMVOA, andan EDFA. The beacon and comms wavelengths pass through a 2-degree offreedom power control, to adjust power to beacon and communicationchannels independently. In an example case, SMVOA could be configured toattenuate either the communication channels or the beacon, while an EDFAamplifies all wavelengths (with approximate equal gain for thesewavelengths), so that the beacon and the communication channels can beset to reach their corresponding setpoints. Furthermore, the system maysupport individual control for balancing of multiple communicationchannels.

In the case that the received power drops on either/both the beaconand/or the communication channels, the remote terminal's SMVOA and EDFA(or equivalent components) are adjusted to compensate for this powerdrop and maintain power near the desired setpoints (up to the limit ofmaximum available power). In the case that the received power increaseson either both the beacon and/or the communication channels, the SMVOAand EDFA are adjusted to compensate for this power increase, andmaintain power near the desired setpoints (down to the limit of theminimum, non-zero achievable power output). Note that it may be morecommon to compensate for a drop in receive power, e.g., due to rain,fog, etc.

In this approach, since a remote terminal acts as a remote sensor forthe local terminal's transmit beam an out-of-band supervisory/managementchannel may be active between the two terminals. However, for certainsituations, an in-band channel would be sufficient.

Given the above, the power control loop technology allows forindependent algorithms that can vary the SMVOA and EDFA (or equivalentcomponents) based on channel and environmental conditions. For example,as explained further below there may be a “Fade” state where the powerdrops below a noise threshold and a “Surge” state where power increasesbeyond bias-free level, as well as one or more “Unstable” states forwind and other special cases that require specific handling of beaconand communication channel power. These states can be triggered bymeasured or inferred knowledge of the channel state and environment. Forinstance, an onboard IMU can be used as an input for the Unstable state.Furthermore, a “Pause” state may be used to handle how the link behaveswhen the system is trying to recover operation during an outage. By wayof example, in the Pause state, the system could perform an automaticrestart and reacquisition of a link alter a long outage such as due topower loss or fog.

The system may be configured to perform obstacle detection, whichinvolves detecting temporary objects. Here, upon detection of atemporary object, the system may not attempt to increase power tocompensate since that object is expected to disappear shortly. Examplesof temporary objects include birds, objects passing through the opticalbeam, ship masts on over-water paths, etc. Obstacle detection uses powerloss and metrics to determine non-weather events. In one example, thesystem may look for uniformity in the drop of all of the wavelengths toensure that this a loss due to an obstacle as opposed to a loss due topointing error or another phenomenon.

If the power fluctuation exceeds a certain bandwidth or magnitudethreshold that is known to fall outside of natural changes occurring inthe atmosphere (e.g., fades due to rain or fog), then the power controlloop process can be held frozen (static) for a certain minimum durationinstead of reacting to the observed power drop. After that duration, thepower available fraction (% of time that full power is available) ismonitored until passing a threshold inside a predetermined duration(e.g., until a solid object has departed), at which point the powercontrol loop would then re-engage and assume that the obstacle haspassed. This approach could be employed in a wide variety of situationsthat distinguish atmospheric events from physical non-atmosphericinterference.

FIG. 6 illustrates an example state diagram 600 of a power control loopin accordance with the above. As shown, there are a number of statesincluding a default state 602, an entry state 604, a rain state 606, anunstable state 608, a fade state 610, a surge state 612 and an extremesurge state 614. The default state here provides for standard operationof the power control loop. According to one aspect, the power controlloop can assess how flesh (current) the incoming data is, andautomatically discard data that is outside a time boundary (e.g., olderthan X seconds or milliseconds). This would account for an out-of-bandcommunication link with extremely high latency, or an in-bandcommunication system where the ARQ is highly active. It can preventadjustment of the power setpoints on data that is no longer relevant tothe current operation of the system.

The entry state 604 that allows for start/stop/pause and updates fromthe main controller of the system. The system would be in this stateduring initial link acquisition, automated recovery, or when the link isdown due to atmospheric conditions. It restores/resets adaptivesetpoints, and can be used to reset EDFA and/or VOA setpoints based onthe automated recovery. It can also prevent adjustment of the poweroutside of that so that the settings do not become unreasonable forre-acquisition of the link when adverse conditions subside. Thus, in oneexample, during automated startup after a terminal power outage, themain controller would evaluate various parameters (e.g., distance fromlink setup, channel temperature and other environmental factors), anddetermine how high to allow the output power to be and independent ofwhat the output power was before the terminal shut down. Thus, in thisexample, if power<threshold, the controller would keep the originalpower, but it power>threshold, it would clip the power at the threshold.

In the rain state 606, the system looks for an error in the trackingsystem where the position feedback appears that tracking is in a goodstate, but the system is unable to maintain sufficient light into thecommunication channel. This may be caused during certain rain conditionswhen the wavefront has multiple peaks/hotspots in power, such as byhaving an excess of transmit power that allows the secondary hotspots tohave enough power that the tracking system is able to lock onto a spotother than the center of the beam. This state can be detected upon astep change in the average delta of receive power between the beacon/PSDand the communication channel. The state can additionally be gated bythe variance of the beacon PSD, with feedback from the pointing error,to distinguish this situation from poor pointing performance that coulddue to high wind or an unstable mount.

In the unstable state 608 (also known as the wind state) it may beexpected that the tracking system in unable to compensate forwind-related disturbances present on the mount. Entry into this statemay be both preemptive and reactive. For instance, the system maypreemptively use the local IMU measurement(s) to enter the wind stateprior to the disturbance of the system moving outside the known boundsof the tracking system (e.g., before wind gusts exceed a threshold). Inthis state, the system can reactively use the variance of the remotereceived power to detect unstable tracking of the remote system. In thewind state, the power readback may not reliable because the beam ismoving on and off the aperture rapidly. In this state, the length of theaverage power may be expanded to account for that. The EDFA power may bedropped and capped to a lower maximum setting to prevent increasingpower due to inaccurate power readback. The rate at which the variableoptical attenuator is controlled can also updated so that the systemdoes not increase the fluctuations of the beacon power as a reaction ofthe beam wander.

The fade state 610 is employed to detect when the update rate of thecontrol of the VOA and/or EDFA may be insufficient to stabilize thereceived power on the link. In this state, the system detects entrybased on the average error of the received power versus the desiredsetpoint of the power control loop. Under normal system operatingconditions (e.g., to the default state 602) an update at this speedcould cause unnecessary adjustments, but in the fade state 610 thisallows the system to up to the maximum adjustable response time of theEDFA and/or VOA in order to maximize the power margin and, stabilize thelink as long as possible when weather conditions are rapidly changing,thereby maximizing the communication system availability. The systemwill exit the fade state when the system is able to maintain thesetpoint or the link goes down due to weather conditions that exceed themargin of the system.

The surge state 612 deals with saturation conditions. Minor saturationmay be due to a weather condition that lifts rapidly, causing thereceived power to spike. Or if the link had previously been down and thesystem suddenly reacquires as the weather lightens up, it can alsoencounter a saturation of power, since the last operating point of thepower setpoints is no longer relevant in present conditions. When thesystem is slightly saturated, the point performance may be suboptimal.In unstable tracking, there can also be inaccurate readback of the powermeasurements. The power control loop in this state can cause the systemto do a number of things to account for this. For instance, the systemcan adjust the update rate of the VOA and decrease the number of powersamples it uses so that it can stabilize the tracking system sooner, andthus provide stable power to the communication system. Additionally,while operating in this state, the system can prevent increase to theEDFA and beacon power levels, which can happen due to power readbackwhen surging, so that the system is not pushed further into a surgecondition.

The extreme surge state 614 can be employed when there is no expectationof reliable feedback of the power, and the tracking system may beunstable. That could lead to degradation of the communication channel,or damage of the communication channel receivers due to excess power andpointing errors that product fast fluctuations on the communicationreceivers, which the system's additional protection mechanism may not beable to compensate for. Similar to the surge state 612, the powercontrol loop in the extreme surge state 614 can cause the system to do anumber of things to account for these issues. For instance, it canadjust the update rate of the VOA and decrease the number of powersamples it uses so that the system can stabilize the tracking systemsooner, and provide stable power the communication system. These aredifferent settings than the minor surge scenario above, which push VOAresponse to a faster rate, but are optimized to prevent instability byadjusting them too fast. Additionally, the extreme surge state 614 canprevent increase to the EDFA and beacon power levels, which can happendue to power readback when surging, so that the system is not pushedfurther into an extreme surge condition.

FIGS. 7A-B show an example of dynamic power adjustment from an operatinglink in accordance with state-based power control as discussed above.FIG. 7A illustrates a plot showing the optical amplifier gain beingadjusted over a range of approximately 20 dB, while the receiveroperating margin remains constant (A). Link conditions continue todeteriorate after the transmitter power is maximized (B). As linkconditions improve, the system reduces the transmitter power to restorethe target operating margin (C). FIG. 7B illustrates correspondingoperating margin across A, B and C, between 0 dBm and 15 dBm. Here, thedouble arrow for (A) illustrates a change in margin in a first timeperiod between t₁ and t₂, the downward arrow for (B) shows that themargin dips as path loss increases around time t₄, and per the upwardarrow for (C) there is a robust recovery at time t₅.

Example Terminal System

FIG. 8 illustrates an example showing a plurality of communicationdevices, such as the first communication device 102 and the secondcommunication device 130, which may be configured to form a plurality ofcommunication links (illustrated as arrows) between a plurality ofcommunication terminals, thereby forming a network 800. The network 800may include client devices 810 and 812, server device 814, andintermediary communication devices 102, 130, 820, 822, and 824 between agiven client device and a server device, or between two client devices.Each of the client devices 810, 812, server device 814, andcommunication devices 820, 822, and 824 may include one or moreprocessors, a memory, a transmitter, a receiver, and a steeringmechanism similar to those described above. Using the transmitter andthe receiver, each communication device in network 800 may form at leastone communication link with another communication device, as shown bythe arrows. The communication links may be for optical frequencies,radio frequencies, other frequencies, or a combination of differentfrequency bands. In FIG. 8 , the communication device 102 is shownhaving communication links with client device 810 and communicationdevices 130, 820, and 822. The communication device 130 is shown havingcommunication links with communication devices 102, 820, 822, and 824.

The network 800 as shown in FIG. 8 is illustrative only, and in someimplementations the network 800 may include additional or differentcommunication terminals. By way of example, the network 800 may be aterrestrial network where the different communication devices arerespectively associated with a plurality of around communicationterminals. In other implementations, the network 800 may includecommunication terminals that are part of one or more high-altitudeplatforms (HAPs), which may be balloons, blimps or other dirigibles,airplanes, unmanned aerial vehicles (UAVs), or any other form ofhigh-altitude platform such as those configured to operate in thestratosphere, or other types of moveable or stationary communicationterminals. Alternatively or additionally, one or more terminals may bedisposed on satellites orbiting the Earth. In some implementations, thenetwork 800 may serve as an access network for client devices such ascellular phones, laptop computers, desktop computers, wearable devices,tablet computers, netbooks, etc. The network 800 also may be connectedto a larger network, such as the Internet, and may be configured toprovide a client device with access to resources stored on or providedthrough the larger computer network.

Example Method

FIG. 9 is a flow diagram 900 illustrating a state-based method ofcontrolling a communication terminal configured to receive free spaceoptical signals. At block 902 the method comprises splitting an inputoptical beam received from another communication terminal into a beaconwavelength and one or more communication wavelengths. At block 904, themethod includes determining target tracking location information basedon beacon information from the beacon wavelength. At block 906 themethod includes attenuating at least one of the one or morecommunication wavelengths, in which the attenuation is adjusted based onthe determined target tracking location information. At block 908 themethod includes outputting one or more detected communication signalsbased on the attenuated at least one of the one or more communicationwavelengths. At block 910 the method includes receiving power adjustmentfeedback from another communication terminal. And at block 912 themethod includes performing state-based power control of thecommunication terminal according to the received power adjustmentfeedback.

Unless otherwise stated, the foregoing alternative examples are notmutually exclusive, but may be implemented in various combinations toachieve unique advantages. As these and other variations andcombinations of the features discussed above can be utilized withoutdeparting from the subject matter defined by the claims, the foregoingdescription of the embodiments should be taken by way of illustrationrather than by way of limitation of the subject matter defined by theclaims. In addition, the provision of the examples described herein, aswell as clauses phrased as “such as,” “including” and the like, shouldnot be interpreted as limiting the subject matter of the claims to thespecific examples; rather, the examples are intended to illustrate onlyone of many possible embodiments. Further, the same reference numbers indifferent drawings can identify the same or similar elements.

The invention claimed is:
 1. A communication terminal configured toreceive free space optical signals, the communication terminalcomprising: a position-sensing detector configured to determine targettracking location information; and a power monitoring block configuredto: receive the determined target tracking location information and tooutput a control signal to adjust an optical attenuator to attenuate atleast one communication wavelength; and perform state-based powercontrol of the communication terminal according to received poweradjustment feedback.
 2. The communication terminal of claim 1, whereinthe power monitoring block of the communication terminal is furtherconfigured to receive one or more detected communication signals outputby at least one photodiode of the communication terminal.
 3. Thecommunication terminal of claim 1, wherein the power monitoring block ofthe communication terminal is further configured to receive the poweradjustment feedback from a power control block of another communicationterminal.
 4. The communication terminal of claim 1, wherein thecommunication terminal further comprises a beam splitter configured tosplit an input optical beam received from another communication terminalinto a beacon wavelength and one or more communication wavelengths. 5.The communication terminal of claim 4, wherein the position-sensingdetector is configured to determine target tracking location informationaccording to the beacon wavelength obtained from the beam splitter. 6.The communication terminal of claim 1, wherein the communicationterminal further comprises at least one photodiode configured to receivethe attenuated at least one communication wavelength and output one ormore detected communication signals.
 7. The communication terminal ofclaim 6, wherein the power monitoring block is further configured toreceive the one or more detected communication signals output by the atleast one photodiode.
 8. The communication terminal of claim 6, furthercomprising the optical attenuator, wherein: the at least onecommunication wavelength is a plurality of communication wavelengths;the at least one photodiode is a plurality of photodiodes eachconfigured to receive one of the plurality of communication wavelengths;and the optical attenuator is configured to separately attenuate each ofthe plurality of communication wavelengths.
 9. The communicationterminal of claim 8, further comprising a demultiplexer configured toreceive each of the plurality of communication wavelengths from theoptical attenuator and to demultiplex the plurality of communicationwavelengths prior to reception by the plurality of photodiodes.
 10. Thecommunication terminal of claim 1, wherein the power monitoring block isconfigured to calculate a center of a focused spot on a sensor plane foran input optical beam.
 11. The communication terminal of claim 1,wherein the received power adjustment feedback is an in-band signal. 12.The communication terminal of claim 1, wherein the received poweradjustment feedback is an out-of-band signal.
 13. The communicationterminal of claim 1, wherein the power monitoring block is furtherconfigured to provide outbound power adjustment feedback to a powercontrol block of another communication terminal.
 14. The communicationterminal of claim 1, wherein the received power adjustment feedbackincludes at least one of a terminal control state, terminal motion, apower statistic, or a tracking statistic.
 15. The communication terminalof claim 1, wherein the state-based power control comprises a defaultstate and multiple discrete states selected from the group consisting ofa rain state, a fade state, a surge state and an unstable state.
 16. Astate-based method of controlling a communication terminal configured toreceive free space optical signals, the method comprising: determiningtarget tracking location information; based on the determined targettracking location information, outputting a control signal to adjust anoptical attenuator to attenuate at least one communication wavelength;and performing state-based power control of the communication terminalaccording to received power adjustment feedback.
 17. The method of claim16, wherein performing the state-based power control includesre-initializing and reacquiring a link with another communicationterminal automatically after loss of power, without human intervention.18. The method of claim 16, wherein the state-based power control isperformed based on (i) at least one of a course pointing mirror angle ora fast steering mirror angle as a starting value, and (ii) at least oneof an amplifier or an attenuator setting for power output.
 19. Themethod of claim 16, wherein the state-based power control includesbounding output power based on at least one of a distance from linksetup or a channel temperature.
 20. The method of claim 16, wherein thestate-based power control comprises a default state and multiplediscrete states selected from the group consisting of a rain state, afade state, a surge state and an unstable state.